View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 24278U 96046B 15027.58952619 -.00000024 00000-0 90467-5 0 5688
2 24278 098.5238 015.5160 0351390 075.4949 036.4194 13.53041962911010
| Epoch (UTC): | 27 January 2015 14:08:55 |
| Eccentricity: | 0.0351390 |
| inclination: | 98.5238° |
| perigee height: | 799 km |
| apogee height: | 1322 km |
| right ascension of ascending node: | 15.5160° |
| argument of perigee: | 75.4949° |
| revolutions per day: | 13.53041962 |
| mean anomaly at epoch: | 36.4194° |
| orbit number at epoch: | 91101 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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